DocumentCode
2643328
Title
Using unknown input observers to detect and isolate sensor faults in a turbofan engine
Author
Dassanake, S.K. ; Balas, Gary J. ; Bokor, Jozsef
Author_Institution
Minnesota Univ., Minneapolis, MN, USA
Volume
2
fYear
2000
fDate
2000
Abstract
An observer based fault detection and isolation method is presented. The method involves combining the unknown input observer theory with the Beard fault detection filter theory to generate a residual signal that has both disturbance decoupling and unidirectional properties. This robust, in the sense of disturbances, residual was used to detect and isolate sensor faults in a turbofan engine model. Finally, the method was successfully extended to detect and isolate sensor faults over a wide range of power input levels by scheduling the observer based on power code
Keywords
aerospace control; aerospace engines; condition monitoring; fault diagnosis; multivariable control systems; observers; robust control; state-space methods; Beard fault detection filter theory; disturbance decoupling; fault detection; fault isolation; full order observer; power code; residual signal; robust residual; sensor faults; state estimation error; state-space matrices; turbofan engine control; unidirectional properties; unknown input observers; weighted output; Actuators; Engines; Equations; Fault detection; Filtering theory; Filters; Observers; Robustness; State estimation; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 2000. Proceedings. DASC. The 19th
Conference_Location
Philadelphia, PA
Print_ISBN
0-7803-6395-7
Type
conf
DOI
10.1109/DASC.2000.884916
Filename
884916
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